ATE438141T1 - Einrichtung zum sicheren betrieb eines flugsteuerstellgliedes eines flugzeugs - Google Patents

Einrichtung zum sicheren betrieb eines flugsteuerstellgliedes eines flugzeugs

Info

Publication number
ATE438141T1
ATE438141T1 AT06830572T AT06830572T ATE438141T1 AT E438141 T1 ATE438141 T1 AT E438141T1 AT 06830572 T AT06830572 T AT 06830572T AT 06830572 T AT06830572 T AT 06830572T AT E438141 T1 ATE438141 T1 AT E438141T1
Authority
AT
Austria
Prior art keywords
movement
actuator
instructions
circuit
movement command
Prior art date
Application number
AT06830572T
Other languages
German (de)
English (en)
Inventor
Bastard Jean-Claude Le
Jean Foisneau
Original Assignee
Thales Sa
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Thales Sa filed Critical Thales Sa
Application granted granted Critical
Publication of ATE438141T1 publication Critical patent/ATE438141T1/de

Links

Classifications

    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P7/00—Arrangements for regulating or controlling the speed or torque of electric DC motors
    • H02P7/06—Arrangements for regulating or controlling the speed or torque of electric DC motors for regulating or controlling an individual dc dynamo-electric motor by varying field or armature current
    • H02P7/18—Arrangements for regulating or controlling the speed or torque of electric DC motors for regulating or controlling an individual dc dynamo-electric motor by varying field or armature current by master control with auxiliary power
    • H02P7/24—Arrangements for regulating or controlling the speed or torque of electric DC motors for regulating or controlling an individual dc dynamo-electric motor by varying field or armature current by master control with auxiliary power using discharge tubes or semiconductor devices
    • H02P7/28—Arrangements for regulating or controlling the speed or torque of electric DC motors for regulating or controlling an individual dc dynamo-electric motor by varying field or armature current by master control with auxiliary power using discharge tubes or semiconductor devices using semiconductor devices
    • H02P7/285—Arrangements for regulating or controlling the speed or torque of electric DC motors for regulating or controlling an individual dc dynamo-electric motor by varying field or armature current by master control with auxiliary power using discharge tubes or semiconductor devices using semiconductor devices controlling armature supply only
    • H02P7/29—Arrangements for regulating or controlling the speed or torque of electric DC motors for regulating or controlling an individual dc dynamo-electric motor by varying field or armature current by master control with auxiliary power using discharge tubes or semiconductor devices using semiconductor devices controlling armature supply only using pulse modulation
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B9/00—Safety arrangements
    • G05B9/02—Safety arrangements electric
    • G05B9/03—Safety arrangements electric with multiple-channel loop, i.e. redundant control systems
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P7/00—Arrangements for regulating or controlling the speed or torque of electric DC motors
    • H02P7/03—Arrangements for regulating or controlling the speed or torque of electric DC motors for controlling the direction of rotation of DC motors
    • H02P7/04—Arrangements for regulating or controlling the speed or torque of electric DC motors for controlling the direction of rotation of DC motors by means of a H-bridge circuit

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Toys (AREA)
  • Electrophonic Musical Instruments (AREA)
  • Jib Cranes (AREA)
  • Selective Calling Equipment (AREA)
AT06830572T 2005-12-13 2006-12-13 Einrichtung zum sicheren betrieb eines flugsteuerstellgliedes eines flugzeugs ATE438141T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0512605A FR2894559B1 (fr) 2005-12-13 2005-12-13 Dispositif de controle securise d'actionneur de commande de vol d'aeronefs
PCT/EP2006/069636 WO2007068711A1 (fr) 2005-12-13 2006-12-13 Dispositif de controle securise d'actionneur de commande de vol d'aeronefs

Publications (1)

Publication Number Publication Date
ATE438141T1 true ATE438141T1 (de) 2009-08-15

Family

ID=37072980

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06830572T ATE438141T1 (de) 2005-12-13 2006-12-13 Einrichtung zum sicheren betrieb eines flugsteuerstellgliedes eines flugzeugs

Country Status (7)

Country Link
US (1) US7711456B2 (fr)
EP (1) EP1960881B1 (fr)
AT (1) ATE438141T1 (fr)
CA (1) CA2633076A1 (fr)
DE (1) DE602006008181D1 (fr)
FR (1) FR2894559B1 (fr)
WO (1) WO2007068711A1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100131123A1 (en) * 2008-11-24 2010-05-27 Honeywell International Inc. Input/steering mechanisms and aircraft control systems
FR2993858B1 (fr) * 2012-07-27 2014-08-22 Thales Sa Procede de regulation en couple d'un actionneur de gouverne commande en position angulaire d'un aeronef a commande de vol mecanique
EP3832424B1 (fr) * 2019-12-02 2022-07-13 Volocopter GmbH Procédé de fonctionnement d'un système d'actionneur, système d'actionneur et aéronef comprenant lesdits procédé et système

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2706153B1 (fr) * 1993-06-07 1995-08-18 Sextant Avionique Dispositif de pilotage automatique pour aérodynes.
DE60141990D1 (de) * 2001-06-29 2010-06-10 Honeywell Int Inc Ausfallpassive servosteuerung
JP2003300473A (ja) * 2002-04-10 2003-10-21 Nsk Ltd 電動パワーステアリング装置
US6919702B2 (en) * 2003-01-16 2005-07-19 Mpc Products Corporation Systems and methods for passivation of servo motors

Also Published As

Publication number Publication date
WO2007068711A1 (fr) 2007-06-21
FR2894559A1 (fr) 2007-06-15
EP1960881A1 (fr) 2008-08-27
EP1960881B1 (fr) 2009-07-29
US20090157238A1 (en) 2009-06-18
FR2894559B1 (fr) 2009-07-10
CA2633076A1 (fr) 2007-06-21
US7711456B2 (en) 2010-05-04
DE602006008181D1 (de) 2009-09-10

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Legal Events

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RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties